Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
CHENG, HSIEN K.
1963.
RECENT ADVANCES IN HYPERSONIC FLOW RESEARCH.
AIAA Journal,
Vol. 1,
Issue. 2,
p.
295.
Simpkins, Peter G.
1963.
On the stable shape of subliming bodies in a high-enthalpy gas stream.
Journal of Fluid Mechanics,
Vol. 15,
Issue. 1,
p.
119.
HOLDEN, MICHAEL S.
1966.
Experimental studies of separated flows at hypersonic speeds. I - Separated flows over axisymmetric spiked bodies..
AIAA Journal,
Vol. 4,
Issue. 4,
p.
591.
Hahn, Mansop
1966.
Pressure distribution and mass injection effects in the transitional separated flow over a spiked body at supersonic speed.
Journal of Fluid Mechanics,
Vol. 24,
Issue. 2,
p.
209.
ALBUM, H. HARVEY
1968.
Regarding the utility of spiked blunt bodies..
Journal of Spacecraft and Rockets,
Vol. 5,
Issue. 1,
p.
112.
GOLDMAN, R. L.
MORKOVIN, M. V.
and
SCHUMACHER, R. N.
1968.
Unsteady control surface loads of lifting re-entry vehicles at very high speeds..
AIAA Journal,
Vol. 6,
Issue. 1,
p.
44.
ALBUM, H. HARVEY
1969.
Hypersonic laminar separation on a cone with slip flow.
AIAA Journal,
Vol. 7,
Issue. 11,
p.
2057.
Panov, Yu. A.
Shvets, A. I.
and
Khazen, A. M.
1970.
Study of base pressure fluctuations behind a cone in supersonic flow.
Fluid Dynamics,
Vol. 1,
Issue. 6,
p.
84.
FLETCHER, L.S.
BRIGGS, D.G.
and
PAGE, R.H.
1970.
A REVIEW OF HEAT TRANSFER IN SEPARATED AND REATTACHED FLOWS.
WYBORNY, WOLFGANG
and
KABELITZ, HANS-PETER
1971.
Comparison of Hypersonic Aerodynamic Deceleration Systems Based on Gun-Tunnel Investigation.
Journal of Spacecraft and Rockets,
Vol. 8,
Issue. 8,
p.
892.
JENKINS, R. B.
TAYLOR, J. P.
BROWNE, T. P.
and
BRIGGS, L. A.
1971.
Astrobee D: An Advanced Technology Meteorological Rocket Vehicle.
Journal of Spacecraft and Rockets,
Vol. 8,
Issue. 8,
p.
895.
Borisenko, V. M.
1972.
Supersonic flow past axisymmetric flared cones.
Fluid Dynamics,
Vol. 4,
Issue. 3,
p.
31.
Avduevskii, V. S.
Gretsov, V. K.
and
Medvedev, K. I.
1972.
Stability of a flow with leading stall zones.
Fluid Dynamics,
Vol. 7,
Issue. 1,
p.
67.
Dan'kov, B. N.
and
Novikov, L. V.
1972.
Unsteady supersonic flow over cone with disk-type skirt.
Fluid Dynamics,
Vol. 3,
Issue. 4,
p.
125.
GOLDMAN, R.
and
OBREMSKI, H.
1973.
Experimental investigation of hypersonic buzz on a high cross-range shuttle configuration.
Abbett, Michael J.
Cooper, Larry
Dahm, Thomas J.
and
Jackson, Michael D.
1975.
Flow Characteristics about Concave Conic Forebodies at M^ = 5.
AIAA Journal,
Vol. 13,
Issue. 11,
p.
1419.
Widhopf, George F.
and
Victoria, Keith J.
1975.
Proceedings of the Fourth International Conference on Numerical Methods in Fluid Dynamics.
Vol. 35,
Issue. ,
p.
431.
Antonov, A. N.
and
Gretsov, V. K.
1976.
Unsteady separated supersonic flow over pointed and spiked bodies.
Fluid Dynamics,
Vol. 9,
Issue. 4,
p.
578.
Demetriades, A.
and
Hopkins, Lt. A.T.
1976.
Asymmetric shock-wave oscillations on spiked bodies of revolution.
Journal of Spacecraft and Rockets,
Vol. 13,
Issue. 11,
p.
703.
MONFORT, A.
FEHL, C.
and
CASSANTO, J.
1976.
An experiment to determine the existence of R/V nose tip transient shocks.